摘要
提出一种适用于导弹总体设计的机电联合仿真方法。在ADAMS/View中建立导弹虚拟样机,在MATLAB/Simulink中构建模块化的仿真系统,通过ADAMS/Controls模块实现虚拟样机和控制系统之间的接口,动力学问题由ADAMS中的求解器进行解算,而控制与相关计算由MATLAB完成。提出了这种仿真方法在进行导弹总体设计时的功能,并举例说明。最后总结了这种方法的特点。
A electromechanieal co-simulation method applied to the preliminary design of missile is presented.The virtual prototype is built with ADAMS/View and the modularized simulation system is with MATLAB/Simulink. The interface between the virtual prototype and control system is the ADAMS/Controls module.The dynamic issues are solved by ADAMS solver,and control algorithms and related computed is completed by MATLAB.The functions of the simulation approach to missile preliminary design are listed and illustrated.In the end,the features of the method are summarized.
出处
《弹箭与制导学报》
CSCD
北大核心
2006年第S5期187-189,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
武器装备预研项目(404050801)
关键词
机电联合仿真
导弹
总体设计
electromechanical co-simulation
missile
preliminary design
